Mechanics of Aerospace Structures - Mechanical and Aerospace Engineering


High spatial resolution stress-sensing materials ebled through the dispersion of no-sensor particles have potentially significant benefits in monitoring structural health and impending failure when integrated with load-bearing structures. Such materials will answer a significant need for noninvasive methods to assess the integrity and quality of carbon-based composites with a surge in their usage as aerospace structures. In this study, stress sensing noparticle-matrix systems will be incorporated with existing carbon-fiber reinforced composites and piezospectroscopic (PS) methods will be used to establish damage detection capabilities.

Project Dates

Start Date: 1/11/2022 - End Date: 4/30/2022

Students Needed

Type of Project

Individual

Student Responsibilities

Experimental and Analytical efforts

Time Commitment

Student Requirements

Interest in experimental mechanics.

Interested in Working With the Following Programs

For EXCEL URE Students Only

Additional Notes

Position Overview

  • Date Posted: 10-11-2017
  • Location:
    • Orlando (Main Campus)
  • Paid: Yes